CN104975946A - Sundial type turbine engine - Google Patents
Sundial type turbine engine Download PDFInfo
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- CN104975946A CN104975946A CN201410659525.6A CN201410659525A CN104975946A CN 104975946 A CN104975946 A CN 104975946A CN 201410659525 A CN201410659525 A CN 201410659525A CN 104975946 A CN104975946 A CN 104975946A
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Abstract
The invention relates to a turbine engine, in particular to a sundial type turbine engine which is designed mainly to solve the problem the existing turbine engine is high in oil consumption. The comprises a box body, cylinder bodies, cylinder covers, spark plugs, pistons, piston rings, connecting rods, an upper cover and a base, wherein the cylinder bodies are fixed on the upper cover; a power output shaft is mounted on the upper cover and the base; a distribution chain wheel, a starter gear and turbine blades are arranged on the power output shaft; a turbine jacket is fixed on the cylinder covers; an exhaust valve on the cylinder cover is connected with an air inlet of the turbine jacket through an exhaust passage; the turbine jacket is provided an exhaust outlet; a cam disc is arranged on a cam disc shaft on the cylinder cover; teeth are formed around the cam disc; an air inlet cam and an exhaust cam are arranged on the cam disc; the cam disc is provided with a chain; the chain is connected with the distribution chain wheel; an inclined disc is arranged on the power output shaft; a bearing is arranged on the inclined disc; connecting rod upper and lower plates are connected with a bearing jacket; spherical surfaces are arranged on the upper surfaces of lower plates; spherical surfaces are arranged on the lower surfaces of upper plates; balls at the lower ends of the connecting rods are arranged in the spherical surfaces between the upper plates and the lower plates; and the upper ends of the connecting rods are connected with the pistons. The sundial type turbine engine has the advantages of less energy consumption.
Description
Technical field:
The present invention relates to a kind of turbogenerator.
Background technique:
Existing turbogenerator comprises main shaft, and main shaft has turbine wheel, is set with turbine cylinder outside turbine wheel, and there is oil nozzle in turbine front, and shortcoming is that fuel consumption is large, and work efficiency is low, and noise is large.
Summary of the invention:
It is few that technical problem to be solved by this invention is to provide a kind of power consumption, and working efficiency is high, the corona formula turbogenerator that noise is little.
Above-mentioned purpose is achieved in that it comprises casing and several cylinder bodies, cylinder body there is cylinder cap, cylinder cap there is spark plug, piston, piston ring is had in each cylinder body, connecting rod is contained on piston by link pin, described casing is cylindrical shape, upper cover is arranged at the top of cylindrical box, base is arranged at the bottom of cylindrical box, several cylinder bodies are fixed on and cover, and be distributed on circumferentially same, pto＝power take-off is contained on the upper cover of cylindrical box and the center hole of base by bearing, pto＝power take-off is equipped with distribution sprocket wheel and starter receiver, pto＝power take-off is also fixed with some turbine blades, turbine overcoat is set with outside turbine blade, turbine overcoat is fixed on cylinder cap, exhaust valve on cylinder cap is connected by the suction port of air outlet flue with turbine overcoat, the opposite side of turbine overcoat is provided with relief opening, each cylinder cap there is cam disk axle, cam disk axle is equipped with cam disk, tooth is had around cam disk, cam disk there are intake cam and exhaust cam, intake valve on cylinder cap is relative with intake cam, exhaust valve on cylinder cap is relative with exhaust cam, enter, exhaust cam is (namely the distance of intake cam and exhaust cam and cam disk axle is unequal) not on same circle, cam disk there is chain be connected with the distribution sprocket wheel on pto＝power take-off, also has the swash plate that circular, circular swash plate is contained on pto＝power take-off by the borehole jack on its center of circle, and be welded and fixed with pto＝power take-off, circular swash plate is apart from the oblique upper of one, two limits in its center of circle farthest, its center of circle, another is in the oblique below of its center of circle opposite side, certain angle is had between the inclined-plane of circular swash plate and pto＝power take-off, its angle is advisable with about 45 °, circular swash plate is equipped with bearing, bearing inner sleeve is connected with circular swash plate, circular connecting rod upper and lower plates is connected with bearing outside, circular connecting rod upper and lower plates is made up of upper plate and lower plate, the lower end of the corresponding each connecting rod of upper surface of lower plate has a sphere, upper plate is fixed in lower plate, also there is a sphere at sphere place in the corresponding lower plate of lower surface of upper plate, there are opening in sphere central authorities on upper plate, there is spheroid the lower end of connecting rod, the spheroid of connecting rod lower end is placed in, in sphere between lower plate, and spheroid and upper, sphere between lower plate has gap, connecting rod stretches out from the opening of the sphere central authorities upper plate, the upper end of connecting rod is connected with piston by wrist pin, when connecting piston and connecting rod with wrist pin, consider the swaying direction of connecting rod, make connecting rod can only along towards pto＝power take-off and dorsad pto＝power take-off direction swing.
Install and use and working principle: by the starter receiver of this device and the gears meshing of Starter during installation.During work, Starter starts, pto＝power take-off rotates, circular swash plate rotates, bearing inner sleeve on circular swash plate rotates, by the upper and lower plates put outside bearing bead subband dynamic bearing, connecting rod, piston moves downward, intake valve on its cylinder cap is opened and is sucked inflammable gas (diesel engine suck), when pto＝power take-off rotates to 180 °, this piston runs to lower dead center from top dead center, IC Intake Valve Closes, then piston runs compression gas in the jar from lower dead center to top dead center, when moving to 360 °, plug ignition (diesel engine fuel injecting), outburst, exhaust valve is opened simultaneously, gas enters air outlet flue, exhaust valve closing, intake valve is opened, gas enters turbine overcoat, promote turbine wheel and rotate workmanship, pto＝power take-off outputting power, gas is discharged from relief opening, pto＝power take-off rotates 180 ° simultaneously, intake valve is opened, descent of piston air-breathing is to lower dead center, IC Intake Valve Closes, pto＝power take-off rotates 180 ° again, piston runs from lower dead center to top dead center, pressure gas, plug ignition (diesel engine fuel injecting), outburst, promotion turbine rotates, reciprocal thus.
Advantage of the present invention is: power consumption is few, and working efficiency is high, and structure is simple, and noise is little.
Accompanying drawing illustrates:
Fig. 1 is structural representation of the present invention;
Fig. 2 is the plan structure schematic diagram of turbine blade and overcoat thereof in the present invention amplified;
Fig. 3 is the schematic diagram of swash plate in the present invention;
Fig. 4 is the schematic top plan view of connecting rod upper and lower plates in the present invention.
Embodiment:
With reference to Fig. 1-4, it comprises casing 25 and several cylinder bodies 3, cylinder body there is cylinder cap 16, cylinder cap there is spark plug 6, piston 4 is had in each cylinder body, piston ring, connecting rod 22 is contained on piston by link pin, unlike the prior art: described casing is cylindrical shape, upper cover 17 is arranged at the top of cylindrical box, base 18 is arranged at the bottom of cylindrical box, several cylinder bodies are fixed on and cover, and be distributed on circumferentially same, pto＝power take-off 21 is contained on the upper cover of cylindrical box and the center hole of base by bearing, distribution sprocket wheel 13 and starter receiver 20 pto＝power take-off be equipped with, pto＝power take-off is also fixed with some turbine blades 14, turbine overcoat 15 is set with outside turbine blade, turbine overcoat is fixed on cylinder cap, exhaust valve 11 on cylinder cap is connected with the suction port of turbine overcoat by air outlet flue 12, the opposite side of turbine overcoat is provided with relief opening, each cylinder cap there is cam disk axle 9, cam disk 8 cam disk axle is equipped with, tooth is had around cam disk, cam disk there are intake cam 7 and exhaust cam 10, intake valve 5 on cylinder cap is relative with intake cam, exhaust valve on cylinder cap is relative with exhaust cam, enter, exhaust cam is (namely the distance of intake cam and exhaust cam and cam disk axle is unequal) not on same circle, cam disk there is chain be connected with the distribution sprocket wheel on pto＝power take-off, also has the swash plate 23 that circular, circular swash plate is contained on pto＝power take-off by the borehole jack on its center of circle, and be welded and fixed with pto＝power take-off, circular swash plate is apart from the oblique upper of one, two limits in its center of circle farthest, its center of circle, another is in the oblique below of its center of circle opposite side, certain angle is had between the inclined-plane of circular swash plate and pto＝power take-off, its angle is advisable with about 45 °, circular swash plate is equipped with bearing 19, bearing inner sleeve is connected with circular swash plate, circular connecting rod upper and lower plates is connected with bearing outside, circular connecting rod upper and lower plates is made up of upper plate 2 and lower plate 24, the lower end of the corresponding each connecting rod of upper surface of lower plate has a sphere, upper plate is fixed in lower plate, also there is a sphere at sphere place in the corresponding lower plate of lower surface of upper plate, there are opening in sphere central authorities on upper plate, there is spheroid 1 lower end of connecting rod, the spheroid of connecting rod lower end is placed in, in sphere between lower plate, and spheroid and upper, sphere between lower plate has gap, connecting rod stretches out from the opening of the sphere central authorities upper plate, the upper end of connecting rod is connected with piston by wrist pin, when connecting piston and connecting rod with wrist pin, consider the swaying direction of connecting rod, make connecting rod can only along towards pto＝power take-off and dorsad pto＝power take-off direction swing.
Claims (1)
1. corona formula turbogenerator, comprise casing (25) and several cylinder bodies (3), cylinder body there is cylinder cap (16), cylinder cap there is spark plug (6), piston (4) is had in each cylinder body, piston ring, connecting rod (22) is contained on piston by link pin, it is characterized in that: described casing is cylindrical shape, upper cover (17) is arranged at the top of cylindrical box, base (18) is arranged at the bottom of cylindrical box, several cylinder bodies are fixed on and cover, and be distributed on circumferentially same, pto＝power take-off (21) is contained on the upper cover of cylindrical box and the center hole of base by bearing, distribution sprocket wheel (13) and starter receiver (20) pto＝power take-off be equipped with, pto＝power take-off is also fixed with some turbine blades (14), turbine overcoat (15) is set with outside turbine blade, turbine overcoat is fixed on cylinder cap, exhaust valve (11) on cylinder cap is connected with the suction port of turbine overcoat by air outlet flue (12), the opposite side of turbine overcoat is provided with relief opening, each cylinder cap there is cam disk axle (9), cam disk (8) cam disk axle is equipped with, tooth is had around cam disk, cam disk there are intake cam (7) and exhaust cam (10), intake valve (5) on cylinder cap is relative with intake cam, exhaust valve on cylinder cap is relative with exhaust cam, enter, exhaust cam is not on same circle, cam disk there is chain be connected with the distribution sprocket wheel on pto＝power take-off, also has the swash plate (23) that circular, circular swash plate is contained on pto＝power take-off by the borehole jack on its center of circle, and be welded and fixed with pto＝power take-off, circular swash plate is apart from the oblique upper of one, two limits in its center of circle farthest, its center of circle, another is in the oblique below of its center of circle opposite side, certain angle is had between the inclined-plane of circular swash plate and pto＝power take-off, circular swash plate is equipped with bearing (19), bearing inner sleeve is connected with circular swash plate, circular connecting rod upper and lower plates is connected with bearing outside, circular connecting rod upper and lower plates is made up of upper plate (2) and lower plate (24), the lower end of the corresponding each connecting rod of upper surface of lower plate has a sphere, upper plate is fixed in lower plate, also there is a sphere at sphere place in the corresponding lower plate of lower surface of upper plate, there are opening in sphere central authorities on upper plate, there is spheroid (1) lower end of connecting rod, the spheroid of connecting rod lower end is placed in, in sphere between lower plate, and spheroid and upper, sphere between lower plate has gap, connecting rod stretches out from the opening of the sphere central authorities upper plate, the upper end of connecting rod is connected with piston by wrist pin.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410659525.6A CN104975946A (en) | 2014-04-12 | 2014-11-08 | Sundial type turbine engine |
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2014101652962 | 2014-04-12 | ||
| CN201410165296 | 2014-04-12 | ||
| CN201410659525.6A CN104975946A (en) | 2014-04-12 | 2014-11-08 | Sundial type turbine engine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104975946A true CN104975946A (en) | 2015-10-14 |
Family
ID=54272839
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410659525.6A Pending CN104975946A (en) | 2014-04-12 | 2014-11-08 | Sundial type turbine engine |
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| Country | Link |
|---|---|
| CN (1) | CN104975946A (en) |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4174684A (en) * | 1977-05-23 | 1979-11-20 | Hallmann Eckhard P | Variable stroke internal combustion engine |
| JPH10238456A (en) * | 1996-12-27 | 1998-09-08 | Sanden Corp | Piston engine and fluid suction and discharge device |
| AU2003201828A1 (en) * | 2002-01-08 | 2003-07-24 | Douglas Marshall Johns | Rotating positive displacement engine |
| CN2567361Y (en) * | 2002-08-12 | 2003-08-20 | 施铁柱 | Reciprocating piston rotation mechanism |
| WO2007117146A1 (en) * | 2006-04-07 | 2007-10-18 | Fuelconsult As | Piston engine |
| CN201041076Y (en) * | 2007-04-03 | 2008-03-26 | 周怀胜 | IC engine |
| CN103711583A (en) * | 2014-01-02 | 2014-04-09 | 刘兴亚 | Circular arc camber gear shaft type engine |
| CN203822455U (en) * | 2014-04-12 | 2014-09-10 | 刘正斌 | Sundial type turbine engine |
-
2014
- 2014-11-08 CN CN201410659525.6A patent/CN104975946A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4174684A (en) * | 1977-05-23 | 1979-11-20 | Hallmann Eckhard P | Variable stroke internal combustion engine |
| JPH10238456A (en) * | 1996-12-27 | 1998-09-08 | Sanden Corp | Piston engine and fluid suction and discharge device |
| AU2003201828A1 (en) * | 2002-01-08 | 2003-07-24 | Douglas Marshall Johns | Rotating positive displacement engine |
| CN2567361Y (en) * | 2002-08-12 | 2003-08-20 | 施铁柱 | Reciprocating piston rotation mechanism |
| WO2007117146A1 (en) * | 2006-04-07 | 2007-10-18 | Fuelconsult As | Piston engine |
| CN201041076Y (en) * | 2007-04-03 | 2008-03-26 | 周怀胜 | IC engine |
| CN103711583A (en) * | 2014-01-02 | 2014-04-09 | 刘兴亚 | Circular arc camber gear shaft type engine |
| CN203822455U (en) * | 2014-04-12 | 2014-09-10 | 刘正斌 | Sundial type turbine engine |
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Application publication date: 20151014 |
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| RJ01 | Rejection of invention patent application after publication |